N78866
Service difficulty reports · 63
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N78866' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N78866' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CALA2026091419408Sign · brokenDOOR 2 OVERHEAD EMERGENCY EXIT SIGN LIGHT HOUSING LOOSE, FOUND DAMAGED MOUNTS, REPLACED THE EXIT SIGN AND PERFORMED EMERGENCY LIGHT OP CHECKED IAW AMM 33-51-00 EMERGENCY LIGHTS AND EXIT SIGNS CHECK GOOD. ALSO PASSENGER AND LAV CALL LIGHTS CHECK GOOD IAW AMM 3SDR CALA2026030314259Door Sill · corrodedR3 DOOR LOWER SILL HAD CORROSION. REPAIRED R3 DOOR LOWER SILL BTWN BS 1310 - 1370 IAW EC/RA 5310-08814.SDR CALA2026021913914Strap · gougedL1 DOOR CUTOUT UPPER SILL INBOARD STRAP GOUGED BY DOOR SURROUND LINER HARDWARE. REPLACED L1 DOOR UPPER SILL INBOARD STRAP REF SRM 51-40-02 AND BOEING DWG 141N8321 SHEET 1.SDR CALA2026021913913Structure · corrodedSIGNS OF CORROSION FOUND AT INNER CHORD UPPER SURFACE APROX. BS 1459, S17R. SEE N/R 003197679 FOR ALL WORK PERFORMED.SDR CALA2026021213723Floorbeam · corrodedFOUND CORROSION ON THE FLOORBEAM AT BS 333.40, BL 0, SEE BAM N/R 003182031 FOR WORK PERFORMED.SDR CALA2025091508914Slide · no discrepancyDOOR 4R SLIDE WILL NOT ARM, OPENED AND CLOSED DOOR 4R. ARMED SLIDE NORMALLY. OPS CHECK GOODSDR CALA2025073007082Bottle · faultedOPERATIONAL TEST OF THE OFF-WING ESCAPE SLIDE PROCEDURE - REMOVED THE RIGHT INFLATION BOTTLE OF RIGHT OFF WING SLIDE SYSTEM DUE TO OPERATIONAL TEST REF AMM TASK 25-65-02-004-002. REPLACED RIGHT BOTTLE , ESCAPE SLIDE, WING REF AMM 25-65-02-404-009. COMPLIED WISDR CALA2025072106750Skin · scratchedLEFT FUSELAGE SKIN APPOX. STA 418 TO STA. 428. HAS SCRATCH IN SKIN BETWEEN STR.17L AND 18L. FWD OF TAT SENSOR. REF LOG PAGE 5581101 BLENDED, REMOVED DAMAGE REF SRM 51-10-02. NEEDS HFEC INSP FOR CRACKS AND ULTRA SOUND INSP. FOR MATERIAL LOSS. REF SRM 53-00-01-SDR CALA2025063006075Control Cable · out of rigON ROLL OUT FOR TAKE OFF CREW REPORTS AC PULLING TO THE RIGHT WITH FULL LH RUDDER PEDAL INOUT ON ROLL OUT FOR TAKE OFF CREW REPORTS AC PULLING TO THE RIGHT WITH FULL LH RUDDER PEDAL INPUT CHECKED RIG OF AFFECTED SYSTEM AND FOUND CABLES NWSA AND NWSB TO BE MISRSDR CALA2025062605911Bulb · burned outMAIN CABIN R3 DOOR EMERGENCY EXIT SIGN HAS ONE BULB OUT. REPLACED THE LAMP L50 IAW AMM 33-51-01-962-001-002. OPS CHECK GOOD FOR L-50 AFTER CHARGING LIGHT IAW B757 AMM 23-51-01-962-001-002.SDR CALA2025062605910Power Supply · failedEMERGENCY EXIT LIGHT BATTERY CHARGER M737 FAILS TEST. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY M737 AND OPS CHECK GOOD REF B757 AMM 33-51-07.SDR CALA2025052004830Lever · failedDURING THE INSTALLATION OF DOOR 4 RIGHT EMERGENCY SLIDE, THE MANUAL ARM/DISARM LEVER FAILED THE OPERATIONAL CHECK DUE TO A BENT GIRT BAR, WHICH CAUSED THE BAR LOCK ASSEMBLY TO BIND. REMOVED AND REPLACED THE DOOR 4 RIGHT EMERGENCY SLIDE GIRT BAR IN ACCORDANCE WSDR CALA2025040703568Light · detached10C EMERGENCY FLOOR LGT HANGING R/R EPL ATTCHMENT HOUSING REF AMM 25-25-00. OPS CHECK GOO. PARTS USED: EMERGENCY LIGHTS - GENERAL VISUAL INSPECTION (ADDED BY EC0300-01601) PROCEDURE - DOOR 3L AISLE EMERGENCY LIGHT AT HANDRAIL. INOP RELAMPED DOOR 3L AISLE EMERSDR CALA2025032803276Lamp · no testEMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - AISLE AREA LIGHT AT SEAT 32CBA INOP RELAMPED PER AMM 33-51-05-002-001 CK OK. PARTS USED: 99-3351-3-0014, QTY :1SDR CALA2025022402460Lamp · no testEMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - #2 LEFT EXIT EMERGENCY LIGHT DOES NOT ILLUMINATE RELAMPED BULB OPERATIONAL CHECK GOOD.PARTS USED: 99-3351-3-0014,QTY :1SDR CALA2025010201752Sensor · faultedR ENG SPEED CARD AND R ENG BLEED OFF AND CTR R FUEL PUMP OFF AT SAME TIME AS RT ENG N3 FLUCTU PER CREW DEBRIEF CTR R FUEL PUMP, R PACK OFF & R ENG BLEED. N3 WAS FLUCTUATING FULL SCALE. PACK WAS FLUCTUATING OFF AND ON. TOTAL FUEL AFTER LADING IS 35.2 REMOVED ANSDR CALA2024101800876Stringer · corrodedPOSIBLE CORROSION ON BELLY SKIN AT STA 1440 AND STR 30. CUTOUT DAMAGE SECTION, SKIN WAS NOT CORRODED. FABRICATED NEW SPLICE AND FILLER SEE TAG R06302 AND 44-0008 FOR WORK ACCOMPLISHED. ALODINE AND PRIMED AND INSTALLED NEW STRINGER SPLICE AND FILLER. REF ECRA 5SDR CALA2023050301315Skin Splice · corrodedCORROSION FOUND IN LAP SPLICE STA 1660 RH SIDE S25R-S26R. NSPECTION THRESHOLD 37500 FLIGHT CYCLES AFTER AIRPLANE DELIVERY R COMES LATER, REF TABLE 206 ZONE A *[6] ALTERNATIVE I *[1]. WOR AND INSPECTOR (RII) QC 68 V932161. OR REPEAT INSPECTION INTERVAL AFTER THSDR CALA2023041901155Unknown · corrodedAFT LOWER CARGO DRAIN MAST DOUBLER AND SUPPORT BRACKETS HAS CORROSION. REMOVED DRAIN MAST DOUBLER AND BLENDED CORROSION FOUND 100% MATERIAL LOSS. FABRICATED AND INSTALLED NEW DOUBLER IAW B757- 300 SRM 51-40-02 PARA 4AND7 AND BOEING DRAWING 146N3700SDR CALA2022091402347None · noneREVERSER UNLOCK INDICATI ON DURING TAKEOFF. REJ ECTED AT AROUND 100KTS. BTS GOT TO 4 AT HIGHEST DEACTIVATED AND SECURED LEFT ENGINE THRUST REVERSER PER MEL DDP IS COMPLIED WITH, PLACED MEL. 7831E. REQUEST MEL. DISPATCH DESK: 3316 NAME: DUY DATE: 08-SEP-22- NOSDR CALA2022082402164Window · openHIGH SPEED ABORT DUE TO FIRST OFFICERS WINDOW COMING OPEN ON TAK EOFF ROLL. HIGH ENERGY STOP INSPECTION COMPLETED ON L/P 9359946. PERFORMED OPERATIONAL CHECK OF F/O''S SLIDING WINDOW REF AMM 56-11-02-715-020. NO FAULTS NOTED AT THIS TIME.SDR CALA2022072001849Brake Sys · warning messageRTO ON 17L AT 125KTS DUE TO HIGH EGT ON BOTH ENGS. BRAKE TEMPS 8 TOGW 229.4 CREW REPORTED A/C WAS ON 1HR BEFORE DEPARTURE, #1 ENG EGT SHOWED 117 BEFORE MOTORING, AND #2 ENG EGT SHOWED 120 BEFORE MOTORING. AT TOP OF COLD RANGE. ALL TIRES WITHIN NORMAL WEAR LIMISDR CALA2022050901196None · inoperativeBOTH UTIL BUS OFF AT THRUST ADVANCEMENT FOR TO ADDING PICTURE REPLACED BPCU REF AMM24-41-03 OPS CHK GOOD NO LATCHED FAULTS IS FOUND ROTABLE PARTS CHANGE WAS INDICATED - TT # 1652441 SN OFF 1433 CONTROL, BUS PO OFF 99-2441-9-0001 1433 ON 99-2441-9-0001 1072SDR CALA2022021400386Cover · missingDOOR-MOUNTED ESCAPE SYSTEM DOOR 3L - A EVACUATION SLIDE PROBLEM WAS ENCOUNTERED WHICH IS NOT COVERED IN THE FAULT CODE DIAGRAMS FA REPORTS EMERGENCY TEST SWITCH PLASTIC PROTECTIVE COVER MISS ING AT DOOR 3L PICTURED ADDED ITEM DOES NOT REQUIRE GUARD,SEE IPC 3SDR CALA2021100601808None · noneSTATUS MSG NOSE A/G DISAGREE REF FIM 32-09 FT 806, CLEANED & INSPECTED THE NLG NOT COMPRESSED SENSORS, NO DEFECTS NOTED. PER FIM 32-09 R&R PSEU. R&R PSEU PER MM 32-09-04 TEST PASSED PER SAME FAULT CODE 32-09004 & 32-09071 ROTABLE PARTS CHANGE WAS INDICATED - SDR CALA2020042400869Frame · dentedB757-53-3-0523. AFT CARGO COMPARTMENT BS1400 S26L FRAME FOUND W ITH A DENT. MEASURED DENT AT AFT CARGO FRAME STA.1400 S26L FOUND TO BE WITH IN LIMITS IAW B757-300 SRM 53-00-07. INSTALLED DENT DOT ECRA 20 60-01042. LOG PAGE WAS CONVERTED TO ELB FORMAT ON MAY 03SDR CALA2020042400867Stringer · cracked(B757-53-3-0559) STA 780+36 STR 16R CRACKED. REF ST-SAA NR 0091790. REMOVED DAMAGE STR AT STA780+36 STR-16R. ACCOMPLISHED PERMANENT REPAIR IAW B757-300 EC/RA 5310-07781 AT STA 780+36. STR-16R AREA FOD FREE WORK ACCOMPLISHED, INSPECTED.SDR CALA2020042400864Frame · cracked(CUSTOMER REQUEST - SUPPORT TASK) FRAME CRACKED AT FASTENER HOLE STATION 1580 BETWEEN STRINGERS 8R AND 9R. REF ST-SAA NR 0092124. CUTOUT CRACK L=1.250 W=1.050 AND INSTALLED PERMANENT REPAIR ON FRAME STA 1580 BETWEEN STRINGER 8R AND 9R IAW B757-3 SRM 53-00-07 RSDR CALA2020042400862Web · cracked(B757-06-3-0374 R-4 DOOR UPPER INNER WEB AFT LIGHTNING HOLE IS C RACKED. REF ST-SAA NR0091847 CHECKED LIMITS TO CRACK AT R4 DOOR UPPER INNER SKIN; L=.25". OUT OF LIMITS IAW B757-300 SRM 52-10-01 ADI, FIG 101 DETAIL XI. ACC OMPLISHED PERMANENT REPAIR IAW ECRA 5SDR CALA2020042400865Frame · cracked(CUSTOMER REQUEST - SUPPORT TASK) FRAME CRACKED AT FASTENER HOLE STATION 1580 BETWEEN STRINGERS 8L AND 9L. REF ST-SAA NR 0092123. CUTOUT CRACK 1.180 X 1.040 AND INSTALLED PERMANENT REPAIR ON FRAME STA 1580 BETWEEN STRINGER 8L AND 9L IAW B757-3 SRM 53-00-07-R8 SDR CALA2020042400859Stringer · cracked(B757-53-3-0559) STA 780+24 STR 16R CRACKED. REF ST-SAA NR 0091789. CHECKED LIMITS TO CRACKED STRINGER 16R AT STA 780+24; L=.40". OU T OF LIMITS IAW B757-300 SRM 53-00-53 ADI, FIG 101,NOTE A, NO CR ACKS ALLOWED. REMOVED, FABRICATED AND INSTALLED NEW STRINGER SSDR CALA2020042400858Stringer · cracked(B757-53-3-0560) STA 780+24 STR 16L CRACKED. REF ST-SAA NR 00917 87. CHECKED LIMITS TO CRACKED STRINGER 16L AT STA 780+24 L+.70"; OUT OF LIMITS IAW B757-300 SRM 53-00-03 ADI. NO CRACKS ALLOWED. REM OVED, FABRICATE AND INSTALLED NEW STRINGER 16L SECTION, P/N: VSDR CALA2020041700845Bracket · cracked(B757-06-3-0354) FWD CARGO DOOR UPPER FWD CORNER BRACKET CRACKED . REF ST-SAA NR 0091474. REMOVED AND REPLACED FWD CARGO DOOR UPPER FWD CORNER BRACKET IAW BOEING DWG 143N6603 REV F, NEW BRACKET PN 03-2711-3-0074 BATCH 0003644086. PO NO.TUA00003491. WORK ACCOMPSDR CALA2020041300832Seal Depressor · dented(B757-06-3-0354) FWD CARGO AFT SEAL DEPRESSOR IS DENTED. REF ST- SAA NR 0091477. FOUND FWD CARGO DOOR AFT SEAL DEPRESSOR AT STA 615 S-20R TO S-25 R OUT OF LIMITS IAW B757-3 SRM 52-30-02 FIG 101 REMOVED, LOCATED AND INSTALLED NEW SEAL DEPRESSOR PN 143N6603-105 SDR CALA2020041700838Stringer · cracked(B757-53-3-0560) STA 780 780+36 STR 16L CRACKED. REF ST-SAA NR 0 091788. FOUND STRINGER 16L AT STA 780+36 OUT OF LIMITS IAW B757-3 SRM 53 -30-03-R1 L=.750 CUTOUT DAMAGE AND INSTALLED PERMANENT REPAIR TO STRINGER 16L AT STA 780+36 IAW B757-3 SRM 53-30-03-R1 FIGSDR CALA2020041700837Crease Beam · corroded(B757-53-3-0557) CREASE BEAM INNER CHORD HAS CORROSION ON UPPER SURFACE,-LEADING UNDER DRAIN PAN AT L-2 LWR SILL, STA 730-740. R EF ST-SAA NR 0091960. FOUND LH CREASE BEAM INNER CHORD AT STA 660 TO 760 OUT OF LIMITS IAW B757-3 SRM 53-30-15-A1 - FIG 101 L=8 W=1SDR CALA2020041300829Strap · corroded(B757-49-3-8083) APU AIR INLET DOOR HOUSING FUSELAGE CUTOUT HAS CORROSION. REF ST-SAA NR 0091780. REMOVED CORROSION AND CHECKED LIMITS TO APU AIR INLET DOOR HOUSING FUSELAGE CUTOUT FWD STRAP L=3.0 W=1.0 D=.050, OUT OF LIMITS. AFT MIDDLE STRAP L=20 W=1.0 D=.055SDR CALA2020041300828Pan · abnormal(B757-53-3-0545) LH SIDE UPPER LOBE FUSELAGE L1 DOOR HANDLE PAN HAS TWO GOUGES. REF ST-SAA NR 0091391. CHECKED LIMITS TO 2EA GOUGES AT LH SIDE UPPER LOBE FUSELAGE L1 DOOR HANDLE PAN L=2.0 W=.10 D=.012. OUT OF LIMITS IAW B757-3 SRM 52-10-01 FIG 101 DETAIL VI ASDR CALA2019020100192Skin · corrodedAFT AREA OF LAV SERVICE PANEL BETWEEN TRIM REINFORCING RING AND SKIN APPEARS TO HAVE CORROSION. LOG LOCKED FOR FERRY FLIGHT 2723-11JAN, HNL HOU, TO ACCOMPLISH REPAIRS. UNLOCKED FOR COMPLIANCE REPAIRED PER ECRA 5360-01501. SEE FLEET CYCLE L/P 9644766 FOR DE TAISDR CALA2019020100191Frame · corrodedREF L/P 9645024 FOUND CROSSION ON FRAME AT STATION 1560 S-27R AND S-28R REF FLEETCYCLE L/P 9645024 FOR ALL WORKED PERFORMED PLACED ON DI P IAW ECRA5360-01501 PAGE 6 OF 12 STEP 7 TO ACCOMPLISH A PERMANE NT REPAIR ON OR BEFORE 24 MONTHS PLANNING TO CONTACT ENGINSDR CALA2018020200442Light · missingDOOR 1L SLIDE LIGHT IS MISSING. INSTALLED MISSING LIGHT.SDR CALA2017090102995Lamp · inoperativeL3 DOOR SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-51-06.SDR CALA2017050801291Transmitter · faultyAT CRUISE 34K FLIGHT LEVEL. EPR COMMAND TO 1.78 EPR ACTUAL NR1 EPR= 1.41 N1=78.7 EGT=545 N2=77 F/F=3.2, NR 2 EPR =1.74 N1=97 EGT=678 N2=89 F/F=5.7, A/T ON/OFF NO CHANGE, EEC ON/OFF NO CHANGE,ALTITUDE CHANGE TO 28K FLT NO CHANGE, NOT ABLE TO ACCELERATE NR 1 ENSDR CALA2015121300994Engine · malfunctionedRIGHT ENG OIL PRESS 0, SHUT DOWN RT ENG. THE OIL PRESS LIGHT CAME ON DURING THE CLIMB. LEVELED OFF, SHUT DOWN & RETURNED. ENG SHUT DOWN FOR 20 MIN. R & R NR 2 ENG IAW WC 19-7100-1-0900 SEQ 10, RAN ENG OPERATIONS CHECKED NORMAL, NO LEAKS NOTED. ROTABLE PARSDR CALA2014080101062Engine · failedLOW SPEED ABORT 80 KNOTS RT ENG OVER TEMP FOR TDR PURPOSES ONLY IAW LP 7750137 FOR ORIGINAL WRITE UP. R & R NR 2 ENG FOR STALLS & VIBRATIONS.SDR CALA2014021100179Floor Panel · corrodedAFT CARGO FLOOR & RAIL HAS HEAVY CORROSION BETWEEN STATION 1360 - 1380, CUT OUT DAMAGED AREA. FABRICATED REPAIRS & INSTALLED REPAIRS AT AFT CARGO FLOOR SIDE PANEL BETWEEN STATION 1360 TO 1580 & RAIL IAW SRM 53-00-53, 51-40-05 & 51-40-02.SDR CALA2014021000170Light · inoperativeEXIT SIGN BULB OUT AFT OF 21DEF. RELAMPED EXIT SIGN AFT AT 21DEF & PERFORMED OPERATIONS CHECKED NORMAL IAW B757 AMM 33-51-10.SDR CALA2014020700162Wire · damagedL1 EMERGENCY LIGHT TEST SWITCH FAILED OPERATIONS CHECK. R & R WIRE W3752-0035-22 SPLICE IAW B757 AMM 33- 51-12 & BSWPM 20-30-12. PERFORMED EMERGENCY LIGHTS TEST SWITCH OPERATIONAL, TEST CHECKED NORMAL IAW B757 AMM 33-51-00.SDR CALA2014020700157Accelerometer · faultyON CLIMB OUT, NR 1 ENG N3 INCREASED TO AMBER, RAN QRH, REDUCED THRUST FROM 89% N1 TO 75% N1 TO REMAIN OUT OF THE AMBER RANGE, DIVERTED TO HNL. R & R AVM ACCELEROMETER IAW AMM 77-31-01 RBN 5109 R & R NR 1ENG N3 TACH GEN IAW AMM 77-12-02.M7165. PERFORMED HIGH SDR CALA2014012700114Web · corrodedB757-53-3-0532 AFT GALLEY SUB FLOOR WEB HAS CORROSION STATION 1681 RBL 52. REMOVED CORROSION AT AFT GALLEY SUB FLOOR WEB, FOUND TO BE OUT LIMITS. FABRICATED REPAIR DOUBLER, TREATED, PRIMED & INSTALLED DOUBLER IAW B757-300 SRM 51-10-02, 53-60-51 & 51-40-02.
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